N485HA
Service difficulty reports · 65
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N485HA' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N485HA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR ASAA2026031463860Windshear Sys · false indication-RTO- REJECTED TAKEOFF TWICE FOR WINDSHEAR WARNINGS. 1ST AT 85 KIAS. 2ND AT 100 KIAS. GROUNDED - YES. A/C INSP C/W PER FIM 05-50- TASK 809. NO DEFECTS NOTED. FCC 1 & 2 R-T-S TEST PASSED PER AMM 22-00-00-741-803. A/C OK FOR SVC.SDR HALA20251015052Accumulator · blownBRAKE PRESSURE LOW PULLING UP TO THE GATE. FOUND LT BRAKE ACCUMULATOR BLOWN. REMOVED AND REPLACED LT BRAKE ACCUMULATOR IAW AMM 32-44-01, OPS & LEAK CHECKED GOOD. OK FOR SERVICE.SDR HALA20240802036Hydraulic Line · leakingATB: L HYD QTY LO CLIMIBING THROUGH 11,000. REMOVED LEAKING HYD LINE PN- 7972138-616 - ROUTED TO HYD SHOP. REPAIRED HYD LINE PER AMM 20-10-01. INSALLATION, OPS + LEAK CHECK PENDING. INSTALLED HYD LINE P/N 7972138-616 PER AMM 20-10-03 OPS CHECK GOOD LEAK CHECK SDR HALA20240228010Line · failedL HYDRACLIC QUANTITY LOSS. REMOVED AND REPLACED HYDRAULIC LINES TO "ANTISKID CONTROL VALVE" PER AMM 32-45-11.PER PILOT SHUT-OFF LH SYSTEM PUMPS AT 5QTS.LEAK CHECK AND OPS CHECK PENDING(02/26/24 25002) PRESSURIZATION ON BOTH HYD SYTEM AND CHECK GOOD ,NO LEAK SDR HALA202310240047Unknown · unknownEMERGENCY PATH LIGHTING ADJACENT TO SEAT 1B NEEDS REPAIR. REMOVED AND REPLACED EMERGENCY PATH LIGHTING ADJACENT TO SEAT 1B PER AMM 31-51-07-200-801.OPS CHECK GOOD. OK FOR SERVICE.SDR HALA2023081400038Hydraulic Line · damagedHYDRAULIC LT PRESSURE LOW AT TOP OF DESCENT FOLLOWED BY HYDRAULIC LT QUANTITY LOW (3.7 INDICATED QUANITY). TRIED TO REPRESSURIZE PER QRH PROCEDURE UNABLE TO REPRESSURIZE. FOUND RIGHT SIDE HYDRAULIC RT PIPELINE DAMAGD. REPLACED RIGHT SIDE HYDRAULIC PIPELINE FORSDR HALA2022123000014Frame · corrodedFRAME TEE CORRODED AT LT 6:10 POSITION. CLEANED AND TREATED IAW SRM 51-10-04. REMAINING THICKNESS .012. REPAIRED PER E105-485299-PERM.SDR HALA2022123000013Floor Support · corrodedFLOOR SUPPORT WAS FOUND WITH SURFACE CORROSION. REMOVED THE FLOOR SUPPORT. FABRICATED A NEW FLOOR SUPPORT IAW DWG 9936534 AND INSTALLED.SDR HALA2020062500133Wire · pulledOPEN - LOUD NOISE ON TAKEOFF ROLL IN AFT OF AIRCRAFT, LEFT AIR CYCLE MACHINE DUCTS BLOWN AND SENSOR AND TEMPERATURE CONTROL WIRES DAMAGED. FOUND DUCTING TO HEAT EXCHANGER MISSING AND WIRING TO (2) TEMP SENSOR ON (2) DUCTING SHEARED. ALSO FOUND TEMP CONTROL SDR HALA2020052700115Slat · unknownOPEN - ON WALK AROUND FOUND LEFT WING NR 5 SLAT STICKING OUT. REPAIR IN WORK.SDR HALA2020050700106Engine · malfunctionedSUP - AIRTURN BACK AFTER TAKE ENG R SYS FAIL. // FAULT REVIEW ENG 2 FAULT CODE 732138. BITE TEST ENG SYS POWER UP TEST PASSED. PERFORMED FIM TASK 73-21 TASK 837 UP TO D(3) IN ACCORDANCE WITH FIM TASK 73-21 TASK 837,NEED TO REPLACE RH ENG PER ENGINEERING REQUESSDR HALA2020042100093Battery · dischargedEMERGENCY EXIT LIGHTS ABOVE ENTRY WAY AND BOTH AFT CENTER EXIT DOOR INTERMITTENT ON AND SHUTS OFF. // REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY REF AMM 33-51-03. OPS CHECK GOOD. OK FOR SERVICE.SDR HALA2020021800037Duct · failedATB - CABIN ALTITUDE ABOVE 18000 RIGHT PACK WENT INOP O2 MASK CABIN DEPLOYED. // REMOVED AND REPLACED DUCT ASSY ABOVE DUCT CHECK VALVE (PART # 5971880-1HAL). LEAK CHECK GOOD. OK FOR SERVICE. PER AMM 21-22-01.SDR HALA2020011400014Eec · malfunctionedDURING CLIMB OUT, "ENG L FADEC ALT" ALERT DISPLAYED. WOULD NOT RESET - ATB. PERFORMED FIM 73-21 TASK 814. OPS CHECK GOOD. FAULT CLEARED. OK FOR SVC. REMOVED AND REPLACED EEC- PER AMM 73-21-01. OPS CHECK GOOD. OK FOR SVC.SDR HALA2020011400013Probe · faultyATB - SELECT FADEC ALTERNATE (L) ILLUMINATED DURING CLIMBOUT - ABOUT 1,300 FEET C/W QRH PROCEDURES, LIGHT DID NOT GO OUT - RETURNED TO HNL. PER FIM 73-21 TASK 814 STEPS A TO D (4) MECH: CONTINUED FROM STEP D.(3)(B). REMOVED AND REPLACED P2/T2 PROBE PER AMM 73SDR HALA2019111200481Tire · out of roundRTO. EXCESSIVE NOSE GEAR VIBRATION FROM 30-60 KNOTS. REJECTED TAKE OFF. // ACCOMPLISHED INSPECTION FOR HIGH ENERGY STOP PER AMM 05-53-01. NOSE TIRES FOUND OUT OF ROUND. REMOVED AND REPLACED NOSE TIRES PER AMM 32-42-01. SPIN CHECK AND SECURITY CHECK OK. LH, P/NSDR HALA2018121700655Light · malfunctionedFLIGHT ATTENDANT REPORTING EMERGENCY LIGHTS FLASHING ON EACH LANDING. CYCLED EMERGENCY PWR LTS SEVERAL TIMES. NO FAULTS NOTED ON GROUND.SDR HALA2018121700654Relay · malfunctionedCABIN EMERGENCY LIGHTS FLICKERED AFTER LANDING AFTER A COUPLED APPROACH. DID NOT FLASH ON A NON COUPLED APPROACH. REMOVED AND REPLACED EMERGENCY POWER RELAY R2-636 PER AMM 24-36-05. FUNCTIONAL TEST OF EMERGENCY POWER SYSTEM PASSED. OK TO CONT SERVICE.SDR HALA2018092200430Trim Motor · intermittentATB / AUTO TRIM FAIL INFLT & STAB OUT OF TRIM DISPLAYED. FOUND ALTERNATE FOUND ALTERNATE STAB TRIM MOTOR INTERMITTENTLY INOP. REMOVED AND REPLACED ALTERNATE TRIM DRIVE MOTOR PER AMM 27-43-01. INTERMITTENTLY INOP. REMOVED AND REPLACED ALTERNATE TRIM DRIVE MOTORSDR HALA2018062000292Warning Message · false activationBLEED AIR RIGHT TEMP HIGH ALERT MESSAGE DURING ANTI-ICE CHECK. ACCOMPLISHED FIM 36-10 TASK 804. PERFORMED PSC BITE PROCEDURE, NO FAULTS WERE OBSERVED. RAN THE NR 2 ENGINE AND PRESSURIZED THE PNEUMATIC SYSTEM IAW 36-00-00-863-803, NO ALERTS AND TM AND TS TEMPSSDR HALA2018062000291Control Cable · out of adjustROLL AXIS ON CONTROL YOKE HAS MUCH MORE THAN USUAL PLAY, CREATING A NULL CONTROL ZONE, ENOUGH TO MAKE THE AUTO PILOT DRIFT. AUTO PILOT DID NOT DISCONNECT. ACCOMPLISHED ADJUSTMENT OF THE AILERON BUSS CABLE SYSTEM IAW AMM 27-10-00. TEST FLIGHT, OPS CHECKED GOOSDR HALA2018060700286Smoke Detector · malfunctionedLAVATORY SMOKE WARNING MESSAGE HAD INTERMITTENT ACTIVATIONS. PERFORMED A SMOKE DETECTOR OPS CHECK. OPS CHECKED GOOD, OK TO CONTINUE.SDR HALA2017081800228Thermocouple · failedAIR TURN BACK. RT ENGINE SYSTEM FAILED, LT ENGINE SYSTEM FAILED ON CLIMB. PERFORMED FIM TASK 77-22-801, NR 1 ENGINE NO DEFECTS, NR 2 ENGINE TURBINE OVERHEAT CHN A/B DISAGREE, R & R TURBINE BEARING OVERHEAT DETECTOR THERMOCOUPLE IAW AMM 77-23-01, OPS GOOD, NSDR HALA2017041400100Shutoff Valve · faultyATB, AIR SYS L PRESS LO INDICATION IN CLIMB OUT ( PRESSURE REGULATOR AND SHUTOFF VALVE (PR ). REMOVED AND
REPLACED LEFT ENGINE PRSOV PILOT VLV PER AMM 36-12-03. OPS CHECK GOOD. DURING ENGINE GROUND RUN RETURNED ACFT TO NORMAL OPERATING STATUS REMOVED PLACARD SDR HALA2016030100064Landing Gear · malfunctionedON FIRST ATTEMPT, GEAR DID NOT COME DOWN. GEAR INDICATIONS ALL RED, ALSO ALL RED ON CONFIGURATION PAGE. 2ND ATTEMPT OK. COMPLIED WITH INSPECTION OF NLG AND MLGS AND SENSORS. COMPLIED WITH RETURN TO SERVICE TEST OF PROXIMITY SENSING ELECTRONIC UNIT. OPS CHECSDR HALA2016012500018Eec · warning messageDURING FLIGHT, SELECT FADEC ALTN FOR RT ENGINE EAD MSG. R & R RT ENGINE ELECTRONIC ENGINE CONTROL MM 73-21-01, RTS AND RUN CK GOOD.SDR HALA2016011400009Tire · damagedRIGHT INBD TIRE TREADING CAME OFF DURING LANDING ROLL OUT. R & R NR 3 MAIN WHEEL TIRE IAW AMM 32-41-01-000-803 & AMM 32-41-01-400-802. ACCOMPLISHED CHECK ON NR 3 MAIN WHEEL TIRE IAW GMM VOL 1, CH 3 1-D AMM 32-42. ACFT OK FOR SERVICE, TIRE PRESSURE OFF 180 PSDR HALA2015100600206Compressor · stalledLEFT ENGINE COMPRESSOR STALL WITH ASSOCIATED ALERT INFLIGHT. HIGH TGT 1055 DEGREES. PERFORMED ENGINE COMPRESSION STALL CHECKLIST AND ENGINE FAIL SHUTDOWN INFLIGHT CHECKLIST. REPLACED LT ENGINE.SDR HALA201507160137Engine · vibrationRT ENGINE HIGH VIBRATION WITH LOUD NOISE. N2 ENGINE VIBRATION PEAK OF 8.0 IN FLIGHT PEAK OF 9.8 BEFORE SHUTOWN, COULD NOT CONTROL VIBRATION LEVEL WITH THROTTLE POSTION. ENGINE NR 2 SHCEDULED FOR REPLACEMENT.SDR HALA0604201500104Slide · unsecureSERVICE DOOR SLIDE CHUTE CAME UNDONE. R & R SERVICE DOOR SLIDE CHUTE MM 25-61-03, OK FOR SERVICE.SDR HALA2014122000213Dcu · malfunctionedAIR DATA HEAT COMPLETE FAILURE AOA, STATIC, PITOT, RAT, RUDDER, AIR TURNBACK. ACCOMPLISHED FIM TASK 30-30, TASK 814. REPLACED AIR DATA HEATER SWITCH IAW WDM 30-31-01 AND REPLACED DCU IAW AMM 31-43-02. OPS CHECKED OF DCU IS OK. OPS CHECKED OF AOA, STATIC, PSDR HALA2014061800087Latch · unsecureDURING CLIMB AT 5000' "ACCESS COMPT DOOR ALERT DISPLAYED, RETURNED TO DEPARTURE. FOUND FWD NOSE ACCESSORY OVAL COMPARTMENT DOOR, 2, LATCHES OPEN. RESECURED FWD NOSE ACCESSORY OVAL COMPARTMENT DOOR, CONDITION AND SECURITY CK OK, PRESSURE CK OK.SDR HALA2014061700087Latch · unsecureDURING CLIMB AT 5000 FT "ACCESS COMPT DOOR ALERT DISPLAYED. FOUND FWD NOSE ACCESSORY OVAL COMPARTMENT DOOR 2 LATCHES OPEN. RESECURED FWD NOSE ACCESSORY OVAL COMPARTMENT DOOR, CONDITION AND SECURITY CK OK, PRESSURE CK OK.SDR HALA2013112000169Warning Message · illuminated"ENGINE LT SYSTEM FAIL" ALERT AFTER ENG START. ACCOMPLISHED FIM 73-21-801, EEC-1 BITE. NO FAULTS NOTED. RTS-PASSED. OK FOR SERVICE. MESSAGE EXTINGUISHED. IAW MOC NEED TO REPLACE NR 1 ENGINE OIL DIFFERENTAL PRESSURE TRANSDUCER CHANNEL "A" AS A PRECAUTION. SDR HALA2013030200027Proximity Sensor · inoperativeLEFT GEAR RED AFTER TAKEOFF, ALL THREE GREEN (NO RED) ON ARRIVAL. KEPT AIRSPEED BELOW 230 KTS. R & R D1-1057 LT MAIN GEAR UP & LATCHED PROXIMITY SENSOR IAW AMM 32-61-02. OPS CHECK OK.SDR HALA2013021800022Actuator · malfunctionedAFTER TAKEOFF, OBSERVED LT MAIN GEAR LIGHT ON. CYCLED THE GEAR IAW ABNORMAL PROCEDURE. OBSERVED TWO MAIN GEAR DOOR LIGHTS ON. SHORTLY THERE AFTER ALL LIGHTS WENT OFF. TROUBLESHOT IAW FIM 32-60-TASK 801 NO FAULT NOTED ON PSEC BITE TEST AND LEAKS FOUND HYD SDR HALA2013020300017Sensor · failedTAIL MANIFOLD FAIL. R & R PODS AND TAIL OVERHEAT DETECTOR SINGLE POINT SENSOR. REF AMM 36-23-01 AND 36-23-10. RTS TEST PASSED. OK FOR SERVICE.SDR HALA2013012800013Warning Light · illuminatedTAIL MANIFOLD FAIL LIGHT ILLUMINATED, RAN CHECKLIST, LIGHT REMAINED ON AFTER LANDING FOR 1 MIN, EXTINGUISHED AND CAME ON ONE MORE TIME FOR 30 SECONDS. OPENSDR HALA2012021000053Compressor · stalledAT 2000' HAD A LEFT ENGINE COMPRESSOR STALL WITH MODERATE VIBRATION, ENGINE SHUTDOWN. REPLACED NR 1 ENG IAW HAL M143-717.SDR HALA2011101500459Wire · unsecureCARGO SMOKE DETECT LIGHTS DO NOT TEST. SECURED WIRE CONNECTION AT S3-830 MASTER DIM & TEST OPS CHECKED OK IAW AMM 33-11-00 & CARGO SMOKE OPS CHECKED OK IAW AMM 26-13-01.SDR HALA2011091700412Seat Track · corrodedCABIN SEAT TRACK STA 44.5 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW SR09530085 REV D APPLIED TOP COAT TO NEW SEAT TRACK. INSTALLED SEAT TRACK IAW DRAWING SR0953008.SDR HALA2011091700411Seat Track · corrodedCABIN SEAT TRACK STA 204, RBL 22 CORRODED OUT OF LIMITS. REMOVED SEAT TRACK IAW SRM 51-40-02. TREATED, PRIMED AND TO COATED SEAT TRACK IAW SRM 51-10-04. INSTALLED SEAT TRACK IAW IAW DWG SR09530085.SDR HALA2011091200417Door Frame · corrodedAFT CARGO COMP DOOR JAMB LWR SIDE HAS SEVERAL SPOTS OF CORROSION. REMOVED CORROSION AT AFT CARGO COMP DOOR JAMB LWR SIDE(PAN). AFTER CORROSION REMOVAL FOUND AREA LWR DOOR JAMB (PAN) OUT OF LIMITS IN REF WITH SRM 53-00-00. ACCOMPLISHED REPAIR FOR DOOR JAMB PASDR HALA2011082400384Warning Light · inoperativeOPEN - AFT LAV FIRE WARNING LIGHT WILL NOT ILLUMINATE WHEN TESTED. (LAV LOCKED-OUT). OK TO CONTINUE IAW MEL 26-14-01.SDR HALA2011041700158Warning Light · illuminatedSPOILER INBD FAIL CAME ON AFTER TURNING OFF HYD PUMPS DURING CLIMB CHECK. REVIEWED LOG FOR LAST 7 DAYS NO SIMILAR OCCURANCE FOUND. GROUND RAN BOTH ENG & CYCLED ALL FLT CONTROLS W/HYD AUX PUMP IN ON/OFF POS. COULD NOT DUPLICATE SAME COND IAW FIM PROCEDURE 27-SDR HALA2011010700013Skin · dentedSMALL CREASE FOUND UNDER FUSELAGE BELOW AFT CARGO DOOR. BLENDED DAMAGED AREA. EDDY CURRENT CK OK, NO CRACK INDICATION. DENT DAMAGE CONDITION 1A IAW DWG SG09530000, SHEET 31. OK AS IS. AREA PRIMED & PAINTED IAW SRM 51-22-01. SILVER DOT APPLIED.SDR HALA2010120200576Engine · failedOPEN - ABORTED TAKE-OFF DUE NR 1 ENGINE FAILED. ENGINE REPLACEMENT STILL IN WORK.SDR HALA2010031500110Unknown · odorF/A'S NOTICED EMERGENCY LIGHTS FLICKER DURING FLIGHT. THEN ON LANDING EMERGENCY LIGHTS FLICKERED AGAIN AND THE FWD F/A'S DETECTED AN ELECTRICAL TYPE OR ELECTRICAL BURNING ODOR . PERFORMED ENG RUN WITH BOTH GEN'S ON LINE NO DEFECTS NOTED. RAN EMERGENCY LIGHTSDR HALA2009101400465Unknown · odorSTRONG CHEMICAL ODOR ON TAKEOFF THAT DECREASED DURING CLIMBOUT ALL A/C SYSTEM INDICATIONS NORMAL. RAN ENGINES WITH BOTH PACKS ON. NO ODOR NOTED. OK FOR SERVICE.SDR HALA2009072900339Via · failedAFTER DEPARTURE EXPERIENCED MAP SHIFT AND NAVIGATION UNREALABLE, NR 2 DU FAILED ALSO. REPLACED NR 1 VIA, GND CHECK OK IAW MM 31-43-00.
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